Basics of Gas Turbine Power Plant

1. SNIST (JNTUH-B.Tech)
BASICS OF GAS TURBINE PLANT
Dr. VIJAYA BHASKAR SIRIVELLA
M.Tech (Mech)., Ph.D (Mech)., Ph.D (Mgmt)
Professor in Mechanical
EngineeringSreenidhi Inst. of Sci. &
Technology Hyderabad

2. Syllabus: GAS TURBINE PLANT
Introduction – classification - construction
– Layout with auxiliaries – Principles of
working of closed and open cycle gas
turbines. Combined Cycle Power Plants
and comparison.

3. INTRODUCTION
 Gas turbines have been used for electricity generation in the
periods of peak electricity demand
 Gas turbines can be started and stopped quickly enabling
them to be brought into service as required to meet energy
demand peaks.
 Small unit sizes and their low thermal efficiency restricted
the opportunities for their wider use for electricity generation.

4. GAS TURBINE
 The Thermal efficiency of the gas turbine is 20 to 30% compared with the
modern steam power plant 38 to 40%.
 In future it is possible to construct efficiencies in and around 45%.
 Following are the fields of Gas Turbine applications:
Power Generation Aviation
Oil and Gas industry Marine Propulsion
 A Gas Turbine is used in aviation and marine fields because it is self
contained, light weight not requiring cooling water and fit into the overall
shape of the structure.
 It is selected for the power generation because of its simplicity, lack of
cooling water, needs quick installation and quick starting.
 It is used in oil and gas industry because of cheap supply of fuel and low
installation cost.
 Limitations of the gas turbine:
1. They are not self starting
2. low efficiencies at part loads
3. non reversibility
4. Higher rotor speeds
5. Low overall plant efficiency.

8. GAS TURBINE
 Gas turbine plant is defined as “ in which the principle of the prime mover
is of the turbine type and the working medium is a permanent gas”.
 Simple gas turbine plant consists of
 Turbine
 Compressor
 Combustor
 Auxiliary devices like starting device, lubricating pump, fuel pump, oil
system and duct system.
 The working fluid is compressed in a compressor which is generally
rotary, multistage type.
 Heat is added to the compressed fluid in the combustion chamber .
 This high energy fluid at high temperature and pressure then expands in the
turbine thereby generating power.
 Part of the energy generated is consumed in driving the compressor and
accessories and the rest is utilized in electrical energy.

9. GAS TURBINE TERMS
 PRESSURE RATIO: It is the ratio of cycle’s highest to its lowest pressure.
Higher pressure at compressor discharge and lowest pressure at compressor
in let pressure. High Pres from Compressor/Low Pres in Comp
 WORK RATIO: It is the ratio of net work output to the total work
developed in the turbine. Network output/Total work
 AIR RATIO: Kg of air entering the compressor inlet per unit of cycle net
output. i.e. kg/kwh
 COMPRESSOR EFFICIENCY: It is the ratio of work needed for ideal
air compression through a given pressure range to work actually used by
the compressor.
Work needed for Ideal air compression/work actually used by compressor
 ENGINE EFFICIENCY : It is the ratio of work actually developed by the
turbine expanding hot power gas through a given pressure range to that
would be yielded for ideal expansion conditions. Actual work/ideal expan
 COMBUSTION EFFICIENCY: It is the ratio of heat actually released by
1 kg of fuel to heat that would be released by complete perfect combustion.
 THERMAL EFFICIENCY: It is the percentage of total energy input
appearing as net work output of the cycle.

10. GAS TURBINE CLASSIFICATION
 There are two basic types of gas turbines – aero derivative and industrial.
 Aero derivative units are aircraft jet engines modified to drive electrical
generators have a maximum output of 40 MW. These can produce full
power within three minutes after start up. They are not suitable for base
load operation.
 Industrial gas turbines range in sizes up to more than 260 MW. Depending
on size, start up can take from 10 to 40 minutes to produce full output.
Industrial gas turbines have a lower capital cost per kilowatt installed than
aero derivative units and, because of their more robust construction, are
suitable for base load operation.

11. GAS TURBINE POWER PLANTS CLASSIFICATION
1.By Application: Jet Propulsion
 Air craft Prop-Jets
Peak Load Unit
Stand by Unit
 Stationary End of Transmission Line Unit
Base Load Unit
Industrial Unit
 Locomotive
 Marine
 Transport
2.By Cycle:
 Open
 Closed
 Semi closed

12. GAS TURBINE POWER PLANTS CLASSIFICATION
3.According to Arrangement:
 Simple
 Single Shaft
 Multi Shaft
 Inter cooled
 Reheat
 Regenerative
 Combination
4.According to combustion:
 Continuous combustion
 Intermittent combustion
5.By Fuel:
 Solid fuel
 Liquid fuel
 Gaseous fuel

13. GAS TURBINE POWER PLANTS
Classification of Gas Turbines
 Constant Pressure combustion Gas Turbine
 Constant volume combustion Gas Turbine
 Aero derivative units are aircraft jet engines modified to drive electrical
generators have a maximum output of 40 MW. These can produce full
power within three minutes after start up. They are not suitable for base
load operation.
 Industrial gas turbines range in sizes up to more than 260 MW. Depending
on size, start up can take from 10 to 40 minutes to produce full output.
Industrial gas turbines have a lower capital cost per kilowatt installed than
aero derivative units and, because of their more robust construction, are
suitable for base load operation
Open Cycle
Closed Cycle

14. Advantages of Gas Turbine Power Plants over Diesel Plants
 Work developed per kg of air is more than diesel plant
 Less vibrations due to perfect balancing and no reciprocating parts
 Less space requirements
 Capital cost is less
 Higher mechanical efficiency
 Running speed of the turbine is large
 Lower installation and maintenance costs
 Torque characteristics of turbine plants are better than diesel plant
 Ignition and lubrication systems are simpler
 Specific Fuel Consumption (SFC) does not increase with time in gas
turbine plant as rapidly in diesel plants
 Poor quality fuel can be used
 Light weigh with reference to Weight to power ratio is less for gas turbine
power plants
 Smoke less combustion is achieved in gas power plants

15. Disadvantages of Gas Turbine Power Plants over Diesel Plants
 Poor part load efficiency
 Special metals and alloys are required for different components
 Special cooling methods required for cooling of turbine blades
 Short life
 Thermal efficiency is low
 Wide operating speeds the fuel control is difficult
 Needs to have speed reduction devices for higher operating speeds of
turbine.
 Difficult to start a gas turbine compared to diesel engine
 Manufacturing of blades is difficult and costly
 Same output gas turbines produces the five times the exhaust gases than IC
engines.

16. Advantages of Gas Turbine Power Plants over Steam Plants
 No ash handling
 Low capital cost and running costs
 Space requirement is less
 Fewer auxiliaries are used
 Can be built relatively quicker
 Can brought on load quickly to support peak loads
 Thermal efficiency of the gas turbine is higher than steam when
working on top temperature (>5500C)
 Gas turbine plants quite economical for short running hours
 Storage of fuel is smaller and handling is easy.
 Less cooling water required for gas turbine plants compared to
steam
 Weight per H.P. is far less
 Can be installed any where
 Control of gas turbine is much easier.

17. Gas Turbine Power Plant Layout with Auxiliaries
Main Components of the Gas
turbine plant layout are
• Gas Turbine
• Compressor
• Combustor
• Intercooler and Generator

18. GAS TURBINE
 Gas Turbine employs blades mounted on a shaft and
enclosed in a casing.
 Flow of the fluid through the turbine is axial and
tangential to the rotor.
 Basic requirements are light weight, high efficiency,
reliability in operation, long working life.
 Large work output can be obtained per stage with high
blade speeds when the blades are designed to sustain
higher temperature.
 More stages of the turbine blades in the gas power plant
helps to reduce the stress in the blades and increase the
overall life of the turbine.
 Gas turbine blades are continuously subjected to the high
temperature gases, so we need to cool the blades for long
life.
 In air cooling the air is passed through the holes provided
through the blade.

19. Simple Gas Turbine

20. Working Principle of Gas Turbine
 Air is compressed(squeezed) to high pressure by a
compressor.
 Then fuel and compressed air are mixed in a
combustion chamber and ignited.
 Hot gases are given off, which spin the turbine wheels.
 Gas turbines burn fuels such as oil, natural gas and
pulverized(powdered) coal.
 Gas turbines have three main parts:
i) Air compressor
ii) Combustion chamber
iii) Turbine

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Gas turbine power plant
Air compressor:
 The air compressor and turbine are mounted at
either end on a common shaft, with the combustion
chamber between them.
 Gas turbines are not self starting. A starting motor
is used.
 The air compressor sucks in air and compresses it,
thereby increasing its pressure.

22. COMPRESSOR
 The axial flow compressors are used in gas turbine installations.
 An axial flow compressor consists of a series of rotor and stator stages
with decreasing diameters along the flow of air.
 The blades are fixed on the rotors and the rotors are fixed on the shaft.
 The stator blades are fixed on the stator casing.
 The stator blades guide the airflow to the next rotor stage coming from
the previous rotor stage.
 The air flows along the axis of the rotor.
 The K.E. is given to the air as it passes through the rotor and part of it
is converted into pressure.
 An axial compressor is capable of delivering the constant volume of air
over varying discharge pressures.
 These are well suited for large capacities at moderate pressures.
 If the impeller of a centrifugal compressor is designed to give an axial
component of velocity at exit, the design becomes a mixed flow type.

23. COMPRESSOR
The Centrifugal Compressor is superior to the axial flow machine in that high
pressure ratio can be obtained in single stage machine, through at the cost of
lower efficiency and increased frontal area.

24. COMBUSTOR

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Gas turbine power plant
Combustion chamber:
 In the combustion chamber, the compressed air
combines with fuel and the resulting mixture is
burnt.
 The greater the pressure of air, the better the fuel air
mixture burns.
 Modern gas turbines usually use liquid fuel, but they
may also use gaseous fuel, natural gas or gas
produced artificially by gasification of a solid fuel.

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Gas turbine power plant
Turbine:
 Hot gases move through a multistage gas
turbine.
 Like in steam turbine, the gas turbine also has
stationary and moving blades.
 The stationary blades
 guide the moving gases to the rotor blades
 adjust its velocity.
 The shaft of the turbine is coupled to a
generator.

27. TYPES OF GAS TURBINE POWER PLANTS
The gas turbine power plants can be classified mainly
into two categories. These are :open cycle gas
turbine power plant and closed cycle gas turbine
power plant.
Open Cycle Gas Turbine Power Plant In this type
of plant the atmospheric air is charged into the
combustor through a compressor and the exhaust of
the turbine also discharge to the atmosphere.
Closed Cycle Gas Turbine Power Plant In this
type of power plant, the mass of air is constant or
another suitable gas used as working medium,
circulates through the cycle over and over again.

28. OPEN CYCLE GAS TURBINE POWER
PLANTAND ITS CHARACTERISTICS
Gas turbines usually operate on an open
cycle
Air at ambient conditions is drawn into the
compressor, where its temperature and
pressure are raised. The high pressure air
proceeds into the combustion chamber,
where the fuel is burned at constant
pressure. The high-temperature gases
then enter the turbine where they expand
to atmospheric pressure while producing
power output.
Some of the output power is used to drive
the compressor.
The exhaust gases leaving the turbine are
thrown out (not re-circulated), causing the
cycle to be classified as an open cycle

29. Methods of Improvement of Thermal
Efficiency of Open Cycle Gas Turbine
Plant
1.Regenerating (Regenerator)
2. Intercooling
3. Reheating

30. Regenerator
 The exhaust gasses
from the turbine carry a
large quantity of heat
with them since their
temperature is far
above the ambient
temperature.
 They can be used to
heat air coming from
the compressor there
by reducing the mass of
fuel supplied in the
combustion chamber.

31. Regenerator

32. Intercooling
 A compressor utilizes
the major percentage of
power developed by the
gas turbine.
 The work required by the
compressor can be
reduced by compressing
the air in two stages and
incorporation a
intercooler between the
two.

33. INTERCOOLER

34. Reheating
 The output of gas
turbine can be
improved by
expanding the gasses
in two stages with a
reheater between the
two.
 The H.P. turbine
drives the compressor
and the LP turbine
provides useful power
output.

35. CLOSED CYCLE GAS TURBINE POWER PLANT
AND ITS CHARACTERISTICS
 The compression and
expansion processes remain
the same, but the combustion
process is replaced by a
constant-pressure heat
addition process from an
external source.
 The exhaust process is
replaced by a constant-
pressure heat rejection
process to the ambient air.

36. 36
Closed cycle gas turbine power plant
A closed cycle gas turbine is a turbine in which the air/working gas is
circulated continuously within the turbine.

37.  The components of this turbine are compressor, heating chamber,
gas turbine which drives the generator and compressor, and a
cooling chamber
 The closed cycle gas turbine works on the principle of Joule’s
or Brayton’s cycle
 In this turbine, the gas is compressed isentropically and
then passed into the heating chamber. The compressor generally
used is of rotary type.
 The compressed air is heated with the help of some external
source and then made to flow over the turbine blades. The turbine
used here is of reaction type.
 The gas while flowing over the blades of the turbine, gets
expanded. From the turbine the gas is passed to the cooling
chamber. Here the gas is cooled at constant pressure with the help
of circulating water to its original temperature.
 Now the gas is again made to flow through the compressor to
repeat the process.
 Here the same gas is circulated again and again in the
working of a closed cycle gas turbine.

38. OPEN CYCLE GAS TURBINE

39.  A simple open cycle gas turbine consists of a compressor,
combustion chamber and a turbine as shown in the below figure.
The compressor takes in ambient fresh air and raises its pressure.
Heat is added to the air in the combustion chamber by burning
the fuel and raises its temperature.
 The heated gases coming out of the combustion chamber are
then passed to the turbine where it expands doing mechanical
work. Some part of the power developed by the turbine is
utilized in driving the compressor and other accessories and
remaining is used for power generation.
 Fresh air enters into the compressor and gases coming out of the
turbine are exhausted into the atmosphere, the working medium
need to be replaced continuously. This type of cycle is known as
open cycle gas turbine plant and is mainly used in majority of
gas turbine power plants as it has many inherent advantages.

40. Merits and Demerits of Closed Loop Cycle
Turbine over Open Loop Cycle turbine
 Merits:
 Higher thermal efficiency
 Reduced size
 No contamination
 Improved heat transmission
 Lesser Fluid friction
 No loss in working medium
 Greater output
 Inexpensive fuel.
 Demerits:
 Complexity
 Large amount of cooling
water is required.
 Dependent System
 Not economical for moving
vehicles as weight /kW
developed is high.
 Requires the use of very
large air heater.

41. Combination of Gas Turbine Cycles
Gas Turbine and Steam Power Plants:
The combination of gas-turbine-steam cycle aims
at utilizing the heat of exhaust gases from the gas
turbine thus, improve the overall plant efficiency.
The popular designs are:
 1. Heating feed water with exhaust gases.
 2. Employing the gases from a supercharged
boiler to expand in the gas turbine.
 3. Employing the gasses as combustion air in the
steam boiler.

42. Heating feed water with exhaust gases.
 The output heat of the gas
turbine flue gas is utilized to
generate steam by passing it
through a heat recovery
steam generator (HRSG), so
it can be used as input heat to
the steam turbine power plant.
 This combination of two power
generation cycles enhances
the efficiency of the plant.
 While the electrical efficiency
of a simple cycle plant power
plant without waste heat
utilization typically ranges
between 25% and 40%, a
CCPP can achieve electrical
efficiencies of 60% and more.

43. Employing the gases from a supercharged boiler to expand in
the gas turbine.
 The boiler furnace works under a
pressure of about 5 bars and the
gases are expanded in the gas
turbine, the exhaust being used to
heat feed water before being
discharged through the stack.
 The heat transfer rate is very high
as compared to conventional boiler
due to high pressure of gases, and
smaller size of steam generator is
needed.
 No need of forced draught fans as
the gases in furnace are already
under pressure.
 Overall improvement in heat rate is
7%.

44. Employing the gases as combustion air in the
steam boiler.
 Exhaust gases are
used as preheated air
for combustion in the
boiler, results in 5%
improvement in heat
rate. The boiler is fed
with supplementary
fuel and air, and is
made larger than
conventional furnace.

45. Combined Gas Turbine and Diesel Power
Plants
 The performance of
diesel engine can be
improved by
combining it with
exhaust driven gas
turbine.
 Three combinations:
1. Turbo charging
2. Gas Generator
3. Compound engine

46. Turbo Charging / Supercharging
 This method is known as
supercharging.
 The exhaust of the diesel
engine is expanded in the
gas turbine and the work
output of the gas turbine
is utilized to run a
compressor which
supplies the pressurized
air to the diesel engine to
increase its output.

47. Gas Generator
 The compressor which
supplies the compressed
air to the diesel engine is
not driven from gas
turbine but from the
diesel engine through
some suitable device.
 The output of diesel
engine is consumed in
driving the air compressor
and gas turbine supplies
the power.

48. Compound Engine
 The air compressor is
driven from both
diesel engine and gas
turbine through a
suitable gearing and
power output is taken
from the diesel engine
shaft.